多约束条件下的制导律研究综述  

Survey on the developments on the guidance law with impact angular constraints

作　　者：孙未蒙[1,2] 刘湘洪[2] 郑志强[1] 

机构地区：[1]国防科技大学机电工程与自动化学院 [2]中国人民解放军92854部队军械修理厂

出　　处：《飞行力学》2010年第2期1-5,共5页Flight Dynamics

基　　金：国家自然科学基金资助(60374006);国防科技大学优秀研究生创新资助(B070304)

摘　　要：随着导弹等制导武器机动能力的增强,制导精度的提高,多约束条件下的制导律研究成为精确制导研究的新热点。简要介绍了多约束条件下的制导问题,重点评述了近年来多约束条件下的制导律研究情况,对目前多约束条件下的制导律设计进行了比较详细的研究,系统分析了各种方法的优缺点,并分析了其可能的研究内容动态和方向,为精确制导技术的发展提供了参考和借鉴。With the tide of improving in flexibility and precision of the air-to-surface missile, the study on guidance laws is cared by researchers in precision guidance. After the guidance with impact angular constraints is presented simply, this paper concentrates on the study of the guidance law with impact angular constraints in recent years. In the paper, various guidance laws with impact angular constraints are introduced in detail. We don＇t only class the articles of guidance law according to the way of design, but also comment on them. Through the trends and direction of the guidance with impact angular constraints are analyzed, the paper can refer the study of the technology of precision guidance.

关 键 词：制导律 多约束条件 导弹 精确制导 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]